Several methods for resampling SMMR Pathfinder data to the EASE-Grid format are compared. The following methods are described and their properties are discussed: drop in the bucket, nearest neighbor, bilinear, cubic convolution, sin(x)/x, inverse distance squared, Backus-Gilbert. Where appropriate each method is simulated by a 2-d transfer function and the frequency response is derived and is used to describe the expected properties of the method. Three methods, drop in the bucket, nearest neighbor, and inverse distance squared are tested on actual data. Sample images at 25km and 2.5km resolution are presented. Each full grid is then summarized by histograms of brightness temperature values and gradients and these are compared to the original input data histograms. For each method, sample data are compared day to day. Each method is compared to a tessellation over a small area for a single orbit. Finally, problems with the data discovered during these tests are outlined.
Assume that the original signal is continuous and band limited. Also, that the original signal can be completely reconstructed from the swath data. The goal then is to determine an interpolation method that will also allow us to reconstruct the original signal. There is no way for us to directly compare the results of any resampled data to the original signal nor even to the swath data. The best we can do is to evaluate the interpolation methods according to their characteristics. The best method I believe is the one that does the least smoothing to the data while adding as little noise as possible.
Of course, there are problems with these assumptions. The "original" original signal was the 2-D brightness temperature signal of the earth. This was sampled by the back and forth scanning of the SMMR instrument. That time continuous signal was then band limited along scan, however it was not band limited across scan. Any across scan signal with spatial frequency greater than 1 cycle per 50km would then be aliased back into the sampled data as noise. A further complication with these assumptions is that the "original" sampled data were themselves resampled along scan so that all channels were coincident with the 37GHz sample locations. The effects of this as to smoothing the data are not studied here.
All data samples that fall within a grid cell are averaged together. This method cannot be simulated by a transfer function and so no frequency response can be derived. Due to the averaging involved with this method it will shift the peaks in the histogram of Tb values if the input histogram is not symmetrical. It will also decrease the occurance of high gradients in the output. The output will appear to be smoothed and will have a different mean value. Also, since no spatial interpolation is done there will be geolocation errors.
Each grid cell is assigned the value of the nearest data sample. The transfer function is a square wave. The frequency response shows a lot of energy outside of the nyquist interval. This would indicate a very noisy output image. Because the input data are not averaged in any way the output histogram of values should closely match the input. However, a noisy transfer will tend to increase the occurance of high gradients in the output. The output image will appear speckled and will have a high incidence of geolocation errors.
A grid cell is located in the sample data coordinate system at (u,v) which is in the middle of a quadilateral of 4 data samples, (i,j), (i+1,j), (i,j+1), (i+1,j+1), where i=(int)u and j=(int)v. First the top two data samples are interpolated and the bottom two data samples are interpolated, then the results of these two interpolations are interpolated. This can also be expressed as a weighted average with weights as follows: w(i,j) = (1 -|u - i|)*(1 - |v - j|). The transfer function is a squared off cone. If the data coordinates of the grid cell are not known then linear interpolation can be approximated by using weights: w(i,j) = (1-d)*(1-d), where d is the distance from the grid cell center to the sample (i,j). The transfer function for this method is a cone. The frequency response for this function has relatively small side lobes, but a fat center lobe which expands beyond nyquist. Because of the averaging this method could shift the histogram of Tb values and decrease the occurance of high gradients. The output will be noticably smoothed.
Cubic convolution is similar to bilinear, but requires 16 surrounding samples and uses cubic splines ratrher than linear interpolation. If the grid cell is at column u in the data then samples at columns i-1, i, i+1, and i+2 are used. Similarly for rows substituting v for u and j for i. Four interpolations are done across each row, then the four results are interpolated. This can also be expressed as a weighted sum: w(x,y) = C(x)*C(y), for x = (i-1, i, i+1, i+2), y = (j-1, j, j+1, j+2), where C(i-1) = p*(1-p)^2, C(i) = 1- 2*p^2 + p^3, C(i+1) = p*(1+p-p^2), C(i+2) = (1-p)*p^2, p = u - i, and similarly for j, let p = v - j. The transfer function is a squared off splash. The frequency response shows a narrow center, flanked by very small side-lobes. Because the transfer function has negative and positive values this method should sharpen the image while not adding significant noise. The histograms of Tb values and gradients for the output should match the input. This technique requires a backwards navigation to determine sample data coordinates for grid cell centers. This is not a simple transformation when relying solely on the data within the SMMR Pathfinder files.
Sine x over x interpolation is a weighted average over any size kernel with weights solely based on the distance of a sample from the grid cell center. The weight is: w(d) = sin(2PId)/(2PId). The transfer function is the classic damped wave rotated about the z-axis. The signal is limited and non-periodic so the expected pair of spikes in the frequency response get smeared out a bit.
Inverse distance squared is another weighted average based on the distance of a sample from the grid cell center. The weight is: 1/d^2. The transfer function is a dimpled spike and the frequency response is a single fat lobe extending well beyond nyquist. Limiting the maximum distance to 1 sample interval (25km) shrinks both the transfer function and the frequency response's center lobe. The is a forward resampling technique which is easily applied and a good alternative to bacwards navigation methods when the relationship of the grid cell location to the sample coordinate space is difficult to back out (as is the case with the SMMR Pathfinder data).
The SSMR swath data were originally sampled at different intervals for each channel. The Pathfinder data have been interpolated along scan to provide coincident measurements for all channels at the original 37GHz locations. Because of this the Backus-Gilbert optimal interpolation technique, used by the SSM/I EASE-Grid resampling method, is not appropriate for the SMMR Pathfinder data. However, it is included here for comparison. The ideal transfer function would be the antenna gain pattern. However backing out the weights for any given location within the sensor field of view is too computationally intensive for routine data processing, so a 16x16 sub-sampled approximation is used. The coefficients for the weighted sum are pre-computed at 1/4 sample and 1/4 scan intervals and the nearest-neighbor to the actual grid cell center is used. Because of this combination the transfer function appears blocky and the frequency response has some side lobe spikes outside of nyquist.
Three interpolation methods were selected for processing of full hemisphere grids. The sample data are all from the Northern hemisphere, for six consecutive days (three "on" periods) chosen arbitrarily (i.e. these were the first data available to me).
These images zoom in to visually assess differences. There are two different views, an all-at-once mosaic or a sequential animation.
Each histogram plot shows the histogram of brightness temperatures for the original input data (all data that fall within the grid and satisfy the local time selection criteria). The other plots show where the histogram of the resampled data deviates from the original histogram. A shift in the peak values will be shown as a bulge in the difference plot.
Each gradient plot shows the histogram of brightness temperature gradients for the original input data (all data that fall within the grid and satisfy the local time selection criteria). The other plots show where the histogram of gradients in the resampled data deviates from the original. An increase in low gradients indicates smoothing. An increase in high gradients indicates noise.
Permanent features should provide good references. These images examine day to day differences in images. Cumulative histogram plots of Tb differences are used to compare interpolation methods. Presumably the best method will have the lowest cummulative error.
To tesselate is to cover with small tiles. Here the term specifically refers to an interpolation method. First, for each point the set of points which are nearer to it than any other point are listed. This collection of sets of points is called the Delauney triangulation. The triangulation is then used to create a smooth surface over the original data. A set of quintic polynomials are used to fit a surface which is smooth and has a smooth first derivative. The values at the grid points are then taken from this surface. Tesselation is a good general solution to the problem of interpolating irregularly sampled data and can easily be adapted to interpolation on a sphere. It is, however, computationally expensive. Here the results of the test interpolation methods are compared to a tessellation over a small area for a single orbit.
While processing the data for these tests I noticed a few things. Since the sensor looks ahead of/behind??? the satellite I didn't want to use the asc/des flag in the header, but wanted to discriminate based on the location of the sample at nadir. When the satellite is ascending toward the north pole, the latitudes should steadily increase and then decrease as the satellite descends. What I found however, is that the orbit wobbles, rapidly shifting back and forth between ascending (increasing latitude) and descending (decreasing latitude) for a few scans. I found this at the poles, but I suspect it wobbles everywhere in the orbit.
Another problem I noticed was that when I tried to run these same tests on the southern hemisphere, I found no ascending data below 40S for any of the sample days. I have not yet explored this further.
Finally, when comparing the daily differences, I had to compare ascending to ascending and descending to descending because there seems to be a systematic along track error in the geolocation. Take a look at this difference image.